Solar Orbiter

European space-based solar observatory

Solar Orbiter
spacecraft in front of the Sun
Artist's impression of the Solar Orbiter orbiting the Sun
Mission typeSolar heliophysics orbiter
OperatorESA / NASA
COSPAR ID2020-010A Edit this at Wikidata
SATCAT no.45167
Websitewww.esa.int
Mission duration7 years (nominal)
+ 3 years (extended)[1][2]
Elapsed: 4 years, 1 month and 21 days
Spacecraft properties
ManufacturerAirbus Defence and Space
Launch mass1,800 kg (4,000 lb)[3]
Payload mass209 kg (461 lb)[4]
Dimensions2.5 × 3.1 × 2.7 m (8 × 10 × 9 ft)[3]
Power180 watts[3]
Start of mission
Launch date10 February 2020, 04:03 UTC[5]
RocketAtlas V 411 (AV-087)[6]
Launch siteCape Canaveral, SLC-41
ContractorUnited Launch Alliance
Entered serviceNovember 2021
(start of main mission)
Orbital parameters
Reference systemHeliocentric
RegimeElliptic orbit
Perihelion altitude0.28 au[6]
Aphelion altitude0.91 au
Inclination24° (nominal mission)
33° (extended mission)
Period168 days
Epoch?
Main
TypeRitchey–Chrétien reflector
Diameter160 mm
Focal length2.5 m
WavelengthsVisible light, ultraviolet, X-rays
Instruments
EPDEnergetic Particle Detector
EUIExtreme Ultraviolet Imager
MAGMagnetometer
METISMulti Element Telescope for Imaging and Spectroscopy Coronagraph
PHIPolarimetric and Helioseismic Imager
RPWRadio and Plasma Waves
SolOHISolar Orbiter Heliospheric Imager
SPICESpectral Imaging of the Coronal Environment
STIXX-ray Spectrometer/Telescope
SWPASolar Wind Plasma Analyser

Insignia for the Solar Orbiter mission.
← CHEOPS
Euclid →
 

The Solar Orbiter (SolO)[7] is a Sun-observing probe developed by the European Space Agency (ESA) with a National Aeronautics and Space Administration (NASA) contribution. Solar Orbiter, designed to obtain detailed measurements of the inner heliosphere and the nascent solar wind, will also perform close observations of the polar regions of the Sun which is difficult to do from Earth. These observations are important in investigating how the Sun creates and controls its heliosphere.

SolO makes observations of the Sun from an eccentric orbit moving as close as ≈60 solar radii (RS), or 0.284 astronomical units (au), placing it inside Mercury's perihelion of 0.3075 au.[8] During the mission the orbital inclination will be raised to about 24°. The total mission cost is US$1.5 billion, counting both ESA and NASA contributions.[9]

SolO was launched on 10 February 2020 from Cape Canaveral, Florida (USA). The nominal mission is planned until the end of 2026, with a potential extension until 2030.

A comparison of the size of the Sun as seen from Earth (left, 1 au) and from the Solar Orbiter spacecraft (0.284 au, right)
The Solar Orbiter structural thermal model shortly before leaving the Airbus Defence and Space facility in Stevenage, UK

Spacecraft

The Solar Orbiter spacecraft is a Sun-pointed, three-axis stabilised platform with a dedicated heat shield to provide protection from the high levels of solar flux near perihelion. The spacecraft provides a stable platform to accommodate the combination of remote-sensing and in situ instrumentation in an electromagnetically clean environment. The 21 sensors were configured on the spacecraft to allow each to conduct its in situ or remote-sensing experiments with both access to and protection from the solar environment. Solar Orbiter has inherited technology from previous missions, such as the solar arrays from the BepiColombo Mercury Planetary Orbiter (MPO). The solar arrays can be rotated about their longitudinal axis to avoid overheating when close to the Sun. A battery pack provides supplementary power at other points in the mission such as eclipse periods encountered during planetary flybys.

The Telemetry, Tracking and Command Subsystem provides the communication link capability with the Earth in X-band. The subsystem supports telemetry, telecommand and ranging. Low-Gain Antennas are used for Launch and Early Orbit Phase (LEOP) and now function as a back-up during the mission phase when steerable Medium- and High-Gain Antennas are in use. The High-Temperature High-Gain Antenna needs to point to a wide range of positions to achieve a link with the ground station and to be able to downlink sufficient volumes of data. Its design was adapted from the BepiColombo mission. The antenna can be folded in to gain protection from Solar Orbiter's heat shield if necessary. Most data will therefore initially be stored in on-board memory and sent back to Earth at the earliest possible opportunity.

The ground station at Malargüe (Argentina), with a 35-metre (115 ft) antenna, is used for 4 to 8 hours/day (effective). ESA's Malargüe ground station will be used for all operations throughout the mission with the ground stations in New Norcia, Australia, and Cebreros, Spain, acting as backup when necessary.[1]

Mission operations

   Solar Orbiter  ·   Mercury  ·   Venus ·   Earth ·   Sun